Experimental Investigation of an NACA 64A010 Airfoil Section with 41 Suction Slots on Each Surface for Control of Laminar Boundary Layer
01.04.1952
Sonstige
Keine Angabe
Englisch
Boundary-layer and stalling characteristics of NACA 64a010 airfoil section
Engineering Index Backfile | 1950
|Engineering Index Backfile | 1950
|Engineering Index Backfile | 1949
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